Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class)

The pilot was conducting an approach to runway 8, during which the left wing contacted the ground approximately 75 feet from the approach end of the runway. The airplane came to rest about 160 feet down the runway, and off the right side. A pilot who landed on runway 26, about 30 minutes prior to the accident flight, stated that the winds were out of the northwest at 15 knots with gusts, and he experienced plus and minus 10 knots on the airspeed while on final approach. The winds 19 miles to the east, at 1045 eastern standard time, were reported from 310 degrees at 15 knots with gusts up to 20 knots. An AIRMET was issued at 0345, with an advisory for occasional moderate turbulence below 8,000 feet. The AIRMET was reissued at 0945, with the added advisory of, 'Low level wind shear potential over the Boston Area Forecast area east of an Erie-Bristol line due to gusty northwesterly surface winds. Conditions ending by 1600.' An FAA Inspector examined the wreckage and found no preimpact anomalies with the airplane.

During flight, the airplane was cruising at flight level 210 in IFR conditions with turbulence and with the wind from about 255 degrees at 70 knots. The airplane drifted off course at about 1600 cst. At 1610:09, after about ten minutes of unrecognized heading changes, the pilot stated '. . . I've lost my gyro.' At 1610:15, the controller issued a no-gyro vector. At 1611:29, as the airplane was still turning (to a heading that would intercept the original course), the pilot stated 'we've lost aLL our instruments . . . please direct me towards VFR.' He was cleared to descend to 14,000 feet. At about that same time, he stated 'we're in trouble' and 'we've lost all vacuum,' then there was no further radio transmission from the airplane. The airplane entered a steep, downward spiraling, right turn. The left outer wing panel separated up and aft (in flight) from overload and impacted the left stabilizer. The airplane crashed, and parts that separated from the airplane were found over a four mile area. Investigation revealed evidence that the HSI heading card can fail without the HDG flag appearing. Although the pilot had reported the loss of instruments and vacuum, examination of the airplane revealed that the engine, flight controls, electrical system, pitot/static system and vacuum systems exhibited continuity. No malfunction was found that would have led to loss of pressurization or hypoxia.

During the preflight briefing, the pilot was informed of reduced visibility and low ceiling in the vicinity of the destination airport, at the approximate time of the planned arrival. Upon arriving in the Atlanta area, the pilot was issued radar vectors to a final for the localizer runway 31 approach. The pilot was also given the current Atlanta altimeter setting, and was cleared for the localizer runway 31 approach. The airplane collided with a 60-foot tall light pole at a nearby baseball complex 2 miles short of the runway. The weather observation from the Hartsfield International Airport indicated that visual weather conditions prevailed at the time of the accident. However, according to a witness at the accident site, the weather conditions were foggy with reduced visibility. The wreckage distribution path was 2,467 feet right of the localizer course. The minimum descent altitude for this approach, using Atlanta's altimeter setting, was 1260 feet. The ground check of the localizer and DME facility was within normal operating range. Examination of the aircraft navigational radios also tested within normal ranges. The average field elevation in the vicinity of the accident site is 800 feet. The pilot's toxicological examinations detected pseudoephedrine (decongestant), phenylpropanolamine (decongestant), and chlorpheniramine (antihistamine). No samples were available to quantify the blood levels of these medications.

The single engine aircraft departed Essen-Mülheim Airport on a private flight to Westerland-Sylt Airport, carrying one passenger and one pilot. While descending to Westerland-Sylt Airport, the pilot encountered poor weather conditions with limited visibility due to fog and snow falls. On approach, the aircraft crashed few km from the airfield, killing both occupants.

Following an uneventful flight from Bern, the pilot started the descent to Zurich-Kloten Airport in relative good weather conditions (scattered 7,000 feet, visibility 5 km, wind from 340° at 4 knots and OAT 20° C). On short final to runway 14, the single engine aircraft entered an uncontrolled descent, struck the ground, lost its left wing and came to rest about 500 metres short of runway threshold. The pilot, sole on board, was killed.

The airplane collided with trees shortly after takeoff and came to rest in a church yard. There were no witnesses to the crash; however, several local residents heard the airplane overfly their homes at a low altitude. One resident stated that he heard the airplane collide with the trees. Another resident stated that he heard the engine operating as the airplane flew low overhead. Both residents reported that reduced visibility hampered their ability to find the wreckage. One resident estimated that the visibility was about 50 to 60 feet. The prescribed takeoff minimums for that airport is 300 feet and 1 mile visibility. Examination of the airplane did not disclose evidence of mechanical malfunction. The pilot, sole on board, was killed.

The single engine airplane departed with two pilots, two passengers, baggage and equipment. At takeoff, the airplane was 955 pounds over the maximum allowable gross weight, and 2 inches beyond the aft c.g. Limit. After 4 hours of flying, the pilot elected to divert to another airport, due to icing conditions. During the descending left turn from base leg to final approach to runway 22, the airplane dropped, struck the ground, and slid 250 feet. The wings were separated from the airplane during the ground slide by two trees. A satisfactory postaccident engine run was completed. The airplane was calculated to be about 600 pounds over the maximum landing weight, and 2 inches beyond the aft c.g. Limit. The air induction lever was in the primary position, and not the required alternate position for icing conditions. The propeller and stall warning heat switches were off. The airplane had been flying in light freezing rain, which the poh stated should be avoided. Severe mixed icing was reported 25 miles northwest of the airport. Winds at the airport were from 150 degrees at 10 knots, gusting to 16 knots. Both pilots were killed and both passengers were seriously injured.

The airplane departed on runway 31 in instrument meteorological conditions (IMC) and turned right to a heading of 090°. Radar contact (arts tag) was acquired about 1 to 2 miles north of the airport. Reportedly, the arts tag would typically be acquired as the airplane climbed through an altitude of about 700 feet agl. Subsequently, the airplane crashed about 2 miles north of the airport. A witness reported hearing a loud engine noise before the plane crashed. The wreckage path was oriented along a westerly heading and over an area of about 380 feet. There was evidence of an in-flight breakup. An outboard portion of the right wing was found about 150 feet from the main impact crater. An examination revealed the right wing had failed near the production seam. The right spar exhibited features 'typical of an upward bending overstress separation.' Examination revealed no other evidence of preimpact aircraft or engine malfunction. The airplane's gross weight was estimated to be about 4,696 pounds; its max limit was 4,300 pounds. The pilot's logbook indicated that he had flown only 2 instrument approaches in the previous 14 months. All three occupants were killed.

Owned by the Federal Office of Civil Aviation (FOCA), the aircraft was dispatched at Sion Airport to perform several local training flight. At the end of the day, a pilot under training and an FOCA inspector decided to complete a local training flight out of Sion Airport. The single engine aircraft took off at 1935LT and the crew completed several touch-and-go maneuvers. Less than an hour later, after takeoff from runway 26, while in initial climb, the engine failed. The crew attempted to make an emergency landing in an open field when the aircraft collided with a car on a street and crashed on the ground. Both pilots escaped with minor injuries while one people in the car was seriously injured. The aircraft and the car were destroyed.